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EP0266765A2 - Lubrication system for a gas turbine engine - Google Patents

Lubrication system for a gas turbine engine Download PDF

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Publication number
EP0266765A2
EP0266765A2 EP87116288A EP87116288A EP0266765A2 EP 0266765 A2 EP0266765 A2 EP 0266765A2 EP 87116288 A EP87116288 A EP 87116288A EP 87116288 A EP87116288 A EP 87116288A EP 0266765 A2 EP0266765 A2 EP 0266765A2
Authority
EP
European Patent Office
Prior art keywords
lubricant
lubrication system
bearing
compressed air
metering device
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP87116288A
Other languages
German (de)
French (fr)
Other versions
EP0266765A3 (en
EP0266765B1 (en
Inventor
Kurt Dipl.-Ing. Steiner
Erich Dipl.-Ing. Schreiber
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
KHD LUFTFAHRTTECHNIK GMBH
Original Assignee
Kloeckner Humboldt Deutz AG
BMW Rolls Royce GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Kloeckner Humboldt Deutz AG, BMW Rolls Royce GmbH filed Critical Kloeckner Humboldt Deutz AG
Publication of EP0266765A2 publication Critical patent/EP0266765A2/en
Publication of EP0266765A3 publication Critical patent/EP0266765A3/en
Application granted granted Critical
Publication of EP0266765B1 publication Critical patent/EP0266765B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16N—LUBRICATING
    • F16N27/00—Proportioning devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16N—LUBRICATING
    • F16N7/00—Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated
    • F16N7/30—Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated the oil being fed or carried along by another fluid

Definitions

  • the invention relates to a lubrication system for a gas turbine engine according to the preamble of claim 1.
  • Such a lubrication system is known from DE-OS 34 03 401.
  • the lubricant is fed to the storage chambers of the gas turbine engine via a pump, excess lubricant being conveyed back from the storage chambers by means of compressed air into the pump which also functions as a centrifugal separator. Since the bearing is cooled at the same time as the lubricant flow, a correspondingly large volume flow is required, which emits the absorbed heat via an oil cooler.
  • the invention has for its object to provide a lubrication system for gas turbine engines that reliably feeds very small amounts of oil to the bearing regardless of existing flight conditions.
  • a precisely metered volume of lubricant is fed to the bearing per unit of time, which is conveyed into the bearing by means of compressed air.
  • the compressed air is advantageously branched off from the compressor air, so that the lubrication system according to the invention can be operated autonomously on a running gas turbine engine while avoiding mechanical pumps.
  • the metering device works without dead volume, so that there are no uncontrolled fluctuations in the lubricant flow that could lead to damage to the bearing.
  • the metering device is formed from a slide which is moved in translation and has a delivery space which can be cycled back and forth between a filling position and a delivery position is.
  • a control device is provided which moves the slide of the metering device via a suitable actuator.
  • the lubrication system according to the invention essentially consists of the components specified in FIG. 1.
  • the lubricant tank 3 is connected to a metering device 5 via a lubricant line 22 in connection, which 20 compressed air from the compressed air source 2 is supplied via a compressed air line.
  • a location of the lubricant tank 3 under the bearing 7 is also advantageous.
  • a predeterminable amount of a volume withdrawn from the lubricant tank is released into the feed line 23 by means of the compressed air in each working cycle, the air / lubricant mixture transported by the compressed air coming directly into the bearing 7 via a feed 6 and the bearing inner ring and there is supplied to the points to be lubricated. Excess lubricant is fed with the supplied compressed air to a vent 8 via a drain 24 designed as a vent line.
  • the lubrication system is controlled by a control unit 1 that, depending on one or more operating parameters of the gas turbine engine or the bearing 7 to be supplied, specifies the cycle of the metering device 5 via a control line 33. It can be advantageous to also report the pressure P of the compressed air source 2 to the control device via a signal line 30 in order to ensure that the metering device is only activated when the minimum pressure required for transporting the metered lubricant is present.
  • an electrical resistance heater PTC
  • Such an electrical resistance heater controls its resistance as a function of the ambient temperature, so that the heater only works at a low ambient temperature in order to ensure a sufficient viscosity of the lubricant.
  • the metering device 5 can be designed according to the exemplary embodiments according to FIGS. 2 and 3.
  • the metering device 5 essentially consists of a slide 12 which is moved translationally in a housing 19 and which has a cylindrical through-bore 11, which is transverse to its direction of movement, as the delivery space.
  • the delivery chamber 11 lies between the compressed air line 20 and the feed line 23, so that a volume of lubricant in the delivery chamber 11 is blown out by the compressed air into the feed line 23 and transported to the bearing 7 with the compressed air.
  • the delivery chamber 11 is connected to the lubricant line 22 from the lubricant tank 3, while the other end of the delivery chamber 11 is closed by the housing 19.
  • the lubricant which is at a low pressure, enters the delivery chamber 11, the Air in the delivery chamber can escape through the fitting gap of the slide 12 in the housing 19 during the filling process. It may be expedient to incorporate a specially provided ventilation groove in the housing 19 or the slide 12 for venting the delivery chamber 11.
  • a rotary slide valve 12a is provided, which forms the core of the metering device 5a.
  • the delivery chamber 11 which is designed as a cylindrical through-bore, connects in the flow path between the compressed air line 20 and the feed line 23, so that lubricant located in the delivery chamber 11 can be blown out by means of the compressed air and conveyed to the bearing 7 as a lubricant mist. If the rotary valve is rotated by 90 °, one end of the delivery chamber 11 is closed by the housing 19 and the other end is congruent with the lubricant line 22 from the lubricant tank 3 (filling position) in order to fill the delivery chamber 11 with the specified volume with lubricant.
  • the translationally moved slide 12 or the rotary slide 12a is alternately switched between the filling position and the conveying position in a predetermined cycle.
  • any quantity of lubricant can thus be supplied to the bearing 7 to be lubricated within predetermined time periods.
  • the metering device according to the invention shown in each case separates a quantity of lubricant defined by the volume of the delivery chamber from the total quantity of lubricant in the lubricant tank and supplies it to the feed line or the bearing 7 without "dead volume".
  • the operation of the lubrication system according to the invention is explained in detail with reference to FIG. 4.
  • the lubricant tank 3 located geodetically above the bearing 7 is acted upon by a low pressure via a compressed air line 21, in which a throttle is preferably provided. In this way, a largely uniform feed to the metering device is ensured regardless of the fill level of the tank.
  • the compressed air is branched off from the compressor 9 of the gas turbine engine and fed directly to the metering device 5 via a compressed air line 20.
  • a feed line 23 also leads from the metering device 5 to the bearing 7 to be lubricated, the feed line 23 opening axially centrally in a hollow bore 16 in the shaft 17 of the gas turbine engine, the opening lying approximately below the bearing 7.
  • Radial openings 18 to the bearing 7 are provided in the shaft 17 in the region of the mouth in the axial hollow bore 16, through which the lubricant entering the cavity flows to the bearing 7. This delivery takes place essentially through the centrifugal force of the rotating shaft 17, a plurality of openings 18 and bores preferably being provided into the lubrication points of the bearing 7 in order to supply sufficient lubricant.
  • a drain 24 (vent line) is provided, which supplies the excess lubricant to a separator 15 together with the outflowing compressor air.
  • the lubricant is retained in the separator 15 and the compressor air is preferably discharged directly into the exhaust duct of the gas turbine engine.
  • a small amount of lubricant is metered out of the lubricant tank 3 by means of the metering device 5 and fed to the hollow bore 16 of the shaft 17 below the bearing 7 by means of compressed air as a lubricant mist.
  • its slide 12 is provided with an actuating rod 14, the free end of which is an anchor in an electromagnetic actuator 10.
  • control unit sends a signal to the actuator 10 via the control line 33, the actuating rod is shifted to the right and pulls the slide 12 against the force of the spring 13 from the illustrated delivery position into the filling position in which the delivery chamber 11 lies below the lubricant line 22.
  • the control unit determines the cycle as a function of operating parameters of the gas turbine engine or of the bearing 7 to be lubricated.
  • the control unit can regulate the heating power of the heater 4 via the control line 32 depending on the temperature of the lubricant in the lubricant tank 3 reported via the signal line 31. so that the lubricant entering the metering device 5 always has the same viscosity, regardless of the prevailing outside temperatures.
  • the heater 4 is expediently arranged in the flow direction of the lubricant shortly before the metering device 5, so that the lubricant once heated does not disadvantageously cool down until it enters the metering device 5.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Rolling Contact Bearings (AREA)

Abstract

The invention relates to a lubrication system for a gas turbine engine having a lubricant tank (3) from which lubricant is fed to the bearing 7 of the engine. In order to be able reliably to meter and supply very small quantities of oil, it is proposed to provide a metering device 5 as the supplying device, the respective metered quantity from which is supplied into the bearing 7 by means of compressed air (Fig. 4). <IMAGE>

Description

Die Erfindung betrifft ein Schmiersystem für ein Gasturbinentreibwerk nach dem Oberbegriff des Anspruchs 1.The invention relates to a lubrication system for a gas turbine engine according to the preamble of claim 1.

Ein derartiges Schmiersystem ist aus der DE-OS 34 03 401 bekannt. Der Schmierstoff wird über eine Pumpe den Lager­kammern des Gasturbinentriebwerks zugeführt, wobei über­schüssiger Schmierstoff mittels Druckluft aus den Lager­kammern in die gleichzeitig als Fliehkraftabscheider ar­beitende Pumpe zurückgefördert wird. Da mit dem Schmier­stoffstrom gleichzeitig das lager gekühlt wird, ist ein entsprechend großer Volumenstrom erforderlich, der über einen Öklühler die aufgenommene Wärme abgibt.Such a lubrication system is known from DE-OS 34 03 401. The lubricant is fed to the storage chambers of the gas turbine engine via a pump, excess lubricant being conveyed back from the storage chambers by means of compressed air into the pump which also functions as a centrifugal separator. Since the bearing is cooled at the same time as the lubricant flow, a correspondingly large volume flow is required, which emits the absorbed heat via an oil cooler.

Bei Mangel- oder Verbrauchsschmiersystemen ist der vorge­sehene Schmierstoffstrom auf die minimal notwendige Menge ausgerichtet, wodurch sich ein sehr kleiner Volumenstrom ergibt. Derartige kleine Volumenströme sind mit Pumpen aber nur schwierig und dann nur unter erhöhtem Aufwand einstellbar, wobei sie aufgrund bestehender Totvolumina der Pumpen erhebliche Schwankungen im Förderstrom auf­treten. Bei Mangel- oder Verbrauchsschmierung können Schwankungen zu einer Unterbrechung der Schmierung und somit zu einem Aufall des lagers führen, da Fördermengen unterhalb der notwendigen Minimalmenge Lagerschäden be­wirken.In the case of inadequate or consumable lubrication systems, the intended lubricant flow is oriented to the minimum amount required, which results in a very small volume flow results. However, such small volume flows are difficult with pumps and can then only be set with increased effort, and because of the existing dead volumes of the pumps they occur considerable fluctuations in the delivery flow. In the event of insufficient or consumption lubrication, fluctuations can lead to an interruption in the lubrication and thus to an abnormality of the bearing, since delivery quantities below the necessary minimum quantity cause bearing damage.

Der Erfindung liegt die Aufgabe zugrunde, ein Schmier­system für Gasturbinentriebwerke zu schaffen, das unab­hängig von bestehenden Fluglagen sehr kleine Ölmengen der Lagerstelle zuverlässig zuführt.The invention has for its object to provide a lubrication system for gas turbine engines that reliably feeds very small amounts of oil to the bearing regardless of existing flight conditions.

Diese Aufgabe wird nach den kennzeichnenden Merkmalen des Anspruchs 1 gelöst.This object is achieved according to the characterizing features of claim 1.

Mit der Dosiervorrichtung wird dem Lager pro Zeiteinheit ein genau dosiertes Volumen an Schmierstoff zugeführt, das mittels Druckluft in das lager gefördert wird. Die Druck­luft ist vorteilhaft von der Verdichterluft abgezweigt, so daß unter Vermeidung von mechanischer Pumpen des erfin­dungsgemäße Schmiersystem an einem laufenden Gasturbinen­triebwerk autark betrieben werden kann. Die Dosiereinrich­tung arbeitet totvolumenfrei, so daß im Schmierstoffstrom keine unkontrollierten Schwankungen auftreten, die zu Schäden am Lager führen könnten.With the dosing device, a precisely metered volume of lubricant is fed to the bearing per unit of time, which is conveyed into the bearing by means of compressed air. The compressed air is advantageously branched off from the compressor air, so that the lubrication system according to the invention can be operated autonomously on a running gas turbine engine while avoiding mechanical pumps. The metering device works without dead volume, so that there are no uncontrolled fluctuations in the lubricant flow that could lead to damage to the bearing.

In Weiterbildung der Erfindung ist vorgesehen, die Dosier­einrichtung aus einem translatorisch bewegten Schieber mit einem Förderraum auszubilden, der taktend zwischen einer Füllstellung und einer Förderstellung hin- und herbewegbar ist. Zur taktenden Betätigung der Dosiereinrichtung ist ein Steuergerät vorgesehen, daß über ein geeignetes Stell­glied den Schieber der Dosiereinrichtung bewegt.In a further development of the invention, it is provided that the metering device is formed from a slide which is moved in translation and has a delivery space which can be cycled back and forth between a filling position and a delivery position is. For cyclical actuation of the metering device, a control device is provided which moves the slide of the metering device via a suitable actuator.

Weitere Merkmale der Erfindung ergeben sich aus den wei­teren Ansprüchen und der folgenden Beschriebung, in der das in den Zeichnungen dargestellte Schmiersystem in ein­zelnen näher beschrieben ist.Further features of the invention result from the further claims and the following description, in which the lubrication system shown in the drawings is described in more detail.

Es zeigt:

  • Fig. 1 Ein Blockschaltbild des erfindungsgemäßen Schmiersystems,
  • Fig. 2 ein Prinzipbild eines ersten Ausführungsbeispiels der im erfindungsgemäßen Schmiersystem verwendeten Dosiereinrichtung,
  • Fig. 3 ein Prinzipbild eines weiteren Ausführungsbeispiels der in dem erfindungsgemäßen Schmiersystem verwendeten Dosiereinrichtung,
  • Fig. 4 eine schematische Darstellung eines Ausführungsbeispiels des erfindungsgemäßen Schmiersystems
It shows:
  • 1 is a block diagram of the lubrication system according to the invention,
  • 2 shows a schematic diagram of a first exemplary embodiment of the metering device used in the lubrication system according to the invention,
  • 3 shows a schematic diagram of a further exemplary embodiment of the metering device used in the lubrication system according to the invention,
  • Fig. 4 is a schematic representation of an embodiment of the lubrication system according to the invention

Das erfindungsgemäße Schmiersystem besteht im wesentlichen aus den in Fig. 1 angegebenen Komponenten. Ein zentraler Schmierstofftank 3, der vorteilhaft geodätisch über dem zu­versorgenden Lager 7 angeordnet ist, wird über eine Druck­luftleitung 21 von einer Druckluftquelle 2 unter einen ge­ringen Druck gesetzt. Der Schmierstofftank 3 steht über eine Schmierstoffleitung 22 mit einer Dosiereinrichtung 5 in Verbindung, der im übrigen über eine Druckluftleitung 20 Druckluft von der Druckluftquelle 2 zugeführt ist. In Abhängigkeit vom Einsatzfall ist auch eine Lage des Schmierstofftanks 3 geodätisch unter dem Lager 7 zweck­mäßig.The lubrication system according to the invention essentially consists of the components specified in FIG. 1. A central lubricant tank 3, which is advantageously arranged geodetically above the bearing 7 to be supplied, is placed under a low pressure by a compressed air source 2 via a compressed air line 21. The lubricant tank 3 is connected to a metering device 5 via a lubricant line 22 in connection, which 20 compressed air from the compressed air source 2 is supplied via a compressed air line. Depending on the application, a location of the lubricant tank 3 under the bearing 7 is also advantageous.

In der Dosiereinrichtung 5 wird in jedem Arbeitstakt eine vorgebbare Menge eines aus dem Schmierstofftank abge­zogenen Volumens mittels der Druckluft in eine Zuführ­leitung 23 abgegeben, wobei das durch die Druckluft trans­portierte Luft-/ Schmierstoffgemisch über eine Zuführung 6 und den Lagerinnenring unmittelbar in das Lager 7 gelangt und dort den zu schmierenden Stellen zugeführt ist. Über­schüssiger Schmierstoff wird mit der zugeführten Druckluft über einen als Entlüftungsleitung ausgebildeten Abfluß 24 einer Entlüftung 8 zugeführt.In the metering device 5, a predeterminable amount of a volume withdrawn from the lubricant tank is released into the feed line 23 by means of the compressed air in each working cycle, the air / lubricant mixture transported by the compressed air coming directly into the bearing 7 via a feed 6 and the bearing inner ring and there is supplied to the points to be lubricated. Excess lubricant is fed with the supplied compressed air to a vent 8 via a drain 24 designed as a vent line.

Das Schmiersystem ist von einem Steuergerät 1 gesteuert, daß in Abhängigkeit eines oder mehrerer Betreibsparameter des Gasturbinentriebwerks bzw. des zu versorgenden Lagers 7 den Takt der Dosiereinrichtung 5 über eine Steuerleitung 33 vorgibt. Es kann vorteilhaft sein, dem Steuergerät über eine Signalleitung 30 ferner den Druck P der Druckluft­quelle 2 zu melden um dafür Sorge zu tragen, daß die Do­siereinrichtung erst dann angesteuert wird, wenn der zum Transport des dosierten Schmierstoffs erforderliche Mini­maldruck ansteht.The lubrication system is controlled by a control unit 1 that, depending on one or more operating parameters of the gas turbine engine or the bearing 7 to be supplied, specifies the cycle of the metering device 5 via a control line 33. It can be advantageous to also report the pressure P of the compressed air source 2 to the control device via a signal line 30 in order to ensure that the metering device is only activated when the minimum pressure required for transporting the metered lubricant is present.

Da die Fließfähigkeit des Schmierstoffs wesentlich von dessen Temperatur abhängt und eine mangelnde Fließfähig­keit Auswirkungen auf eine genaue Dosierung hat, ist vor­gesehen, zwischen dem Schmierstofftank 3 und der Dosier­einrichtung 5 eine Heizung 4 anzuordnen, die in einem dar gestellten Ausführungsbeispiel über eine Steuerleitung 32 in Abhängigkeit der über eine Signalleitung 31 dem Steuer­gerät gemeldeten Temperatur T des Schmierstoffs im Schmierstofftank 3 angesteuert ist.Since the fluidity of the lubricant depends largely on its temperature and a lack of fluidity has an effect on accurate metering, provision is made to arrange a heater 4 between the lubricant tank 3 and the metering device 5, which is in one embodiment is controlled via a control line 32 as a function of the temperature T of the lubricant in the lubricant tank 3 reported to the control unit via a signal line 31.

Es kann vorteilhaft sein, als Heizung 4 eine elektrische Widerstandsheizung (PTC) vorzusehen, die lediglich an eine Spannungsquelle anzuschließen ist. Eine derartige elektrische Widerstandsheizung regelt ihren Widerstand in Abhängigkeit der umgebungstemperatur, so daß nur bei niedriger Umgebungstemperatur die Heizung arbeitet um eine ausreichende Viskosität des Schmierstoffs sicherstellen.It may be advantageous to provide an electrical resistance heater (PTC) as the heater 4, which is only to be connected to a voltage source. Such an electrical resistance heater controls its resistance as a function of the ambient temperature, so that the heater only works at a low ambient temperature in order to ensure a sufficient viscosity of the lubricant.

Die Dosiereinrichtung 5 kann gemäß den Ausführungsbei­spielen nach den Figuren 2 und 3 ausgeführt sein.The metering device 5 can be designed according to the exemplary embodiments according to FIGS. 2 and 3.

Im Ausführungbeispiel nach Figur 2 besteht die Dosierein­richtung 5 im wesentlichen aus einem in einem Gehäuse 19 translatorisch bewegten Schieber 12, der eine - quer zu seiner Bewegungsrichtung liegende - zylindrische durch­gehende Bohrung 11 als Förderraum aufweist. In der in Fig. 2 gezeigten Förderstellung liegt der Förderraum 11 zwischen der Druckluftleitung 20 und der Zuführleitung 23, so daß ein im Förderraum 11 befindliches Volumen an Schmierstoff durch die Druckluft in die Zuführleitung 23 ausgeblasen und mit der Druckluft zum Lager 7 transpor­tiert wird. Wird der Schieber - im Ausführungsbeispiel nach Fig. 2 nach rechts - in Füllstellung verschoben, ist das eine Ende des Förderraums 11 mit der Schmierstofflei­tung 22 vom Schmierstofftank 3 verbunden, während das an­dere Ende des Förderraums 11 durch das Gehäuse 19 ver­schlossen ist. Der unter einem geringen Druck stehende Schmierstoff tritt in den Förderraum 11 ein, wobei die Luft im Förderraum während des Füllvorgangs durch den Pas­sungsspalt des Schiebers 12 im Gehäuse 19 entweichen kann. Es kann zweckmäßig sein, zur Entlüftung des Förderraums 11 eine speziell vorgesehene Lüftungsnut im Gehäuse 19 oder dem Schieber 12 einzuarbeiten.In the exemplary embodiment according to FIG. 2, the metering device 5 essentially consists of a slide 12 which is moved translationally in a housing 19 and which has a cylindrical through-bore 11, which is transverse to its direction of movement, as the delivery space. In the delivery position shown in FIG. 2, the delivery chamber 11 lies between the compressed air line 20 and the feed line 23, so that a volume of lubricant in the delivery chamber 11 is blown out by the compressed air into the feed line 23 and transported to the bearing 7 with the compressed air. If the slide - in the exemplary embodiment according to FIG. 2 to the right - is moved to the filling position, one end of the delivery chamber 11 is connected to the lubricant line 22 from the lubricant tank 3, while the other end of the delivery chamber 11 is closed by the housing 19. The lubricant, which is at a low pressure, enters the delivery chamber 11, the Air in the delivery chamber can escape through the fitting gap of the slide 12 in the housing 19 during the filling process. It may be expedient to incorporate a specially provided ventilation groove in the housing 19 or the slide 12 for venting the delivery chamber 11.

Im Ausführungsbeispiel nach Fig. 3 ist ein Drehschieber 12a vorgesehen, der das Kernstück der Dosiereinrichtung 5a bildet. In einer ersten Stellung (Förderstellung) liegt der als zylindrische Durchgangsbohrung ausgebildete För­derraum 11 verbindend im Strömungsweg zwischen der Druck­luftleitung 20 und der Zuführleitung 23, so daß im Förder­raum 11 befindlicher Schmierstoff mittels der Druckluft ausgeblasen und als Schmierstoffnebel zum Lager 7 ge­fördert werden kann. Wird der Drehschieber um 90° ver­dreht, so wird ein Ende des Förderraums 11 durch das Ge­häuse 19 verschlossen und das andere Ende gelangt deckungsgleich mit der Schmierstoffleitung 22 vom Schmier­stofftank 3 (Füllstellung), um den Förderraum 11 vorge­gebenen Volumens mit Schmierstoff zu füllen.In the exemplary embodiment according to FIG. 3, a rotary slide valve 12a is provided, which forms the core of the metering device 5a. In a first position (delivery position), the delivery chamber 11, which is designed as a cylindrical through-bore, connects in the flow path between the compressed air line 20 and the feed line 23, so that lubricant located in the delivery chamber 11 can be blown out by means of the compressed air and conveyed to the bearing 7 as a lubricant mist. If the rotary valve is rotated by 90 °, one end of the delivery chamber 11 is closed by the housing 19 and the other end is congruent with the lubricant line 22 from the lubricant tank 3 (filling position) in order to fill the delivery chamber 11 with the specified volume with lubricant.

Mittels des Steuergerätes 1 (Fig. 1) und eines geeigneten Stellgliedes wird der translatorisch bewegte Schieber 12 bzw. der Drehschieber 12a in einem vorgegebenen Takt zwischen der Füllstellung und der Förderstellung wechselnd geschaltet. Durch Änderung des Taktes (und/oder des Vo­lumens des Förderraums 11) können somit beliebige Schmier­stoffmengen innerhalb vorgegebener Zeitspannen dem zu schmierenden Lager 7 zugeführt werden. Hervorzuheben ist, daß die gezeigte erfindungsgemäße Dosiereinrichtung je­weils eine durch das Volumen des Förderraums definierte Schmierstoffmenge von der Gesamtmenge des Schmierstoffs im Schmierstofftank trennt und ohne "Totvolumen" der Zuführ­leitung bzw. dem Lager 7 zuführt.By means of the control device 1 (FIG. 1) and a suitable actuator, the translationally moved slide 12 or the rotary slide 12a is alternately switched between the filling position and the conveying position in a predetermined cycle. By changing the cycle (and / or the volume of the delivery chamber 11), any quantity of lubricant can thus be supplied to the bearing 7 to be lubricated within predetermined time periods. It should be emphasized that the metering device according to the invention shown in each case separates a quantity of lubricant defined by the volume of the delivery chamber from the total quantity of lubricant in the lubricant tank and supplies it to the feed line or the bearing 7 without "dead volume".

Anhand der Fig. 4 ist die Funktionsweise des erfindungsge­mäßen Schmiersystems im einzelnen erläutert. Der geodä­tisch über dem Lager 7 liegende Schmierstofftank 3 wird über eine Druckluftleitung 21, in der vorzugsweise eine Drossel vorgesehen ist, mit einem geringen Druck beauf­schlagt. Auf diese Weise ist unabhängig von der Füllhöhe des Tanks eine weitgehend gleichmäßige Zuführung zur Do­siereinrichtung gewährleistet.The operation of the lubrication system according to the invention is explained in detail with reference to FIG. 4. The lubricant tank 3 located geodetically above the bearing 7 is acted upon by a low pressure via a compressed air line 21, in which a throttle is preferably provided. In this way, a largely uniform feed to the metering device is ensured regardless of the fill level of the tank.

Die Druckluft ist dabei vom Verdichter 9 des Gasturbinen­triebwerks abgezweigt und über eine Druckluftleitung 20 der Dosiereinrichtung 5 unmittelbar zugeführt. Von der Do­siereinrichtung 5 führt ferner eine Zuführleitung 23 zum zu schmierenden Lager 7, wobei die Zuführleitung 23 axial zentral in einer Hohlbohrung 16 der Welle 17 des Gastur­binentriebwerks mündet, wobei die Mündung etwa unterhalb des Lagers 7 liegt. In der Welle 17 sind im Bereich der Mündung in der axialen Hohlbohrung 16 radiale Öffnungen 18 zur Lager 7 vorgesehen, durch die der in den Hohlraum ein­tretende Schmierstoff zum Lager 7 fließt. Diese Förderung erfolgt im wesentlichen durch die Fliehkraft der rotier­enden Welle 17, wobei zur ausreichenden Schmierstoffver­sorgung vorzugsweise eine Vielzahl von Öffnungen 18 und Bohrungen bis in die Schmierstellen des lagers 7 hinein vorgesehen sind.The compressed air is branched off from the compressor 9 of the gas turbine engine and fed directly to the metering device 5 via a compressed air line 20. A feed line 23 also leads from the metering device 5 to the bearing 7 to be lubricated, the feed line 23 opening axially centrally in a hollow bore 16 in the shaft 17 of the gas turbine engine, the opening lying approximately below the bearing 7. Radial openings 18 to the bearing 7 are provided in the shaft 17 in the region of the mouth in the axial hollow bore 16, through which the lubricant entering the cavity flows to the bearing 7. This delivery takes place essentially through the centrifugal force of the rotating shaft 17, a plurality of openings 18 and bores preferably being provided into the lubrication points of the bearing 7 in order to supply sufficient lubricant.

Im radial äußeren Bereich des Lagers 7 ist ein Abfluß 24 (Entlüftungsleitung) vorgesehen, die den überschüssigen Schmierstoff zusammen mit der abströmenden Verdichterluft einem Abscheider 15 zuführt. Im Abscheider 15 wird der Schmierstoff zurückgehalten und die Verdichterluft vor­zugsweise unmittelbar in den Abgasschacht des Gasturbinen­triebwerks abgeführt.In the radially outer area of the bearing 7, a drain 24 (vent line) is provided, which supplies the excess lubricant to a separator 15 together with the outflowing compressor air. The lubricant is retained in the separator 15 and the compressor air is preferably discharged directly into the exhaust duct of the gas turbine engine.

Um eine Mangel- oder Verbrauchsschmierung des Lagers 7 ohne mechanisch angetriebene Ölpumpe zu gewährleisten, wird mittels der Dosiervorrichtung 5 eine kleine Schmier­stoffmenge dosiert aus dem Schmierstofftank 3 abgezogen und mittels Druckluft als Schmierstoffnebel der Hohl­bohrung 16 der Welle 17 unterhalb des Lagers 7 zugeführt. Zum Betrieb der Dosiereinrichtung 5 ist deren Schieber 12 mit einer Betätigungsstange 14 versehen, deren freies Ende als Anker in einem elektromagnetischen Stellglied 10 liegt. Gibt das Steuergerät über die Steuerleitung 33 ein Signal an das Stellglied 10, wird die Betätigungsstange nach rechts verschoben und zieht den Schieber 12 gegen die Kraft der Feder 13 von der dargestellten Förderstellung in die Füllstellung in der der Förderraum 11 unterhalb der Schmierstoffleitung 22 liegt.In order to ensure a lack of lubrication or consumption lubrication of the bearing 7 without a mechanically driven oil pump, a small amount of lubricant is metered out of the lubricant tank 3 by means of the metering device 5 and fed to the hollow bore 16 of the shaft 17 below the bearing 7 by means of compressed air as a lubricant mist. To operate the metering device 5, its slide 12 is provided with an actuating rod 14, the free end of which is an anchor in an electromagnetic actuator 10. If the control unit sends a signal to the actuator 10 via the control line 33, the actuating rod is shifted to the right and pulls the slide 12 against the force of the spring 13 from the illustrated delivery position into the filling position in which the delivery chamber 11 lies below the lubricant line 22.

Das Steuergerät bestimmt den Takt in Abhängigkeit von Be­triebsparametern des Gasturbinentriebwerks bzw. des zu schmierenden Lagers 7. Darüber hinaus kann das Steuergerät in Abhängigkeit von der über die Signalleitung 31 ge­meldete Temperatur des Schmierstoff im Schmierstofftank 3 die Heizleistung der Heizung 4 über die Steuerleitung 32 regeln, damit der in die Dosiereinrichtung 5 eintretende Schmierstoff - unabhängig von anstehenden Außentempera­turen - immer dieselbe Viskosität aufweist. Die Heizung 4 ist hierzu zweckmäßig in Flußrichtung des Schmierstoffs kurz vor der Dosiereinrichtung 5 angeordnet, so daß der einmal erwärmte Schmierstoff bis zum Eintreten in die Do­siereinrichtung 5 nicht nachteilig abkühlt.The control unit determines the cycle as a function of operating parameters of the gas turbine engine or of the bearing 7 to be lubricated. In addition, the control unit can regulate the heating power of the heater 4 via the control line 32 depending on the temperature of the lubricant in the lubricant tank 3 reported via the signal line 31. so that the lubricant entering the metering device 5 always has the same viscosity, regardless of the prevailing outside temperatures. For this purpose, the heater 4 is expediently arranged in the flow direction of the lubricant shortly before the metering device 5, so that the lubricant once heated does not disadvantageously cool down until it enters the metering device 5.

Claims (10)

1. Schmiersystem für ein Gasturbinentriebwerk, mit einem Schmierstofftank (3) und einer Fördervorrichtung, die Schmierstoff von dem Schmierstofftank zu mindest einem Lager (7) des Triebwerks fördert, wobei das Lager (7) zu­mindest einen Abfluß (24) aufweist, über den mittels dem Lager (7) zugeführter Druckluft, überschüssiger Schmier­stoff abgeführt ist,
dadurch gekennzeichnet, daß die Fördervorrichtung aus einer Dosiereinrichtung (5) für den Schmierstoff besteht, dessen jeweilige Dosiermenge mittels Druckluft in den Be­reich der Lagerstelle (7) förderbar ist.1. Lubrication system for a gas turbine engine, with a lubricant tank (3) and a conveying device that conveys lubricant from the lubricant tank to at least one bearing (7) of the engine, the bearing (7) having at least one drain (24) via which compressed air supplied to the bearing (7), excess lubricant is removed,
characterized in that the conveying device consists of a metering device (5) for the lubricant, the respective metered amount of which can be conveyed into the region of the bearing point (7) by means of compressed air. 2. Schmiersystem nach Anspruch 1,
dadurch gekennzeichnet, daß die Dosiereinrichtung (5) einen Förderraum (11) vorgegebenen Volumens aufweist, der taktend mit Schmierstoff füll- und entleerbar ist.2. Lubrication system according to claim 1,
characterized in that the metering device (5) has a delivery space (11) of predetermined volume, which can be filled and emptied in cycles with lubricant. 3. Schmiersystem nach Anspruch 2,
dadurch gekennzeichnet, daß der Förderraum (11) als zylindrische Bohrung ausgebildet ist, die in Förder­stellung an einem Ende mit einer druckluftführenden Lei­tung (20) und gleichzeitig an ihrem axial anderen Ende mit der Zuführleitung (23) zur Lagerstelle (7) verbunden ist und in Füllstellung an einem Ende mit dem Schmierstofftank (3) verbunden ist, wobei gleichzeitig das andere Ende ver schlossen ist.3. Lubrication system according to claim 2,
characterized in that the delivery chamber (11) is designed as a cylindrical bore which, in the delivery position, has a compressed air-carrying line (20) at one end and at the same time at its axially other end the feed line (23) to the bearing point (7) is connected and in the filling position is connected at one end to the lubricant tank (3), the other end being closed at the same time. 4. Schmiersystem nach Anspruch 2 oder 3,
dadurch gekennzeichnet, daß der Förderraum (11) in einem translatorisch bewegten Schieber (12) angeordnet ist.4. Lubrication system according to claim 2 or 3,
characterized in that the conveying space (11) is arranged in a translationally moved slide (12). 5. Schmiersystem nach Anspruch 2 oder 3,
dadurch gekennzeichnet, daß der Förderraum (11) in einem Drehschieber (12a) angeordnet ist.5. Lubrication system according to claim 2 or 3,
characterized in that the delivery chamber (11) is arranged in a rotary slide valve (12a). 6. Schmiersystem nach einem der Ansprüche 1 bis 5,
dadurch gekennzeichnet, daß die Druckluft ein Teilstrom der Verdichterluft ist.6. Lubrication system according to one of claims 1 to 5,
characterized in that the compressed air is a partial flow of the compressor air. 7. Schmiersystem nach einem der Ansprüche 1 bis 6,
dadurch gekennzeichnet, daß der Takt der Dosiereinrichtung (5) von einem Steuergerät (1) vorzugsweise in Abhängigkeit mehrerer Betriebsparameter des Gasturbinentriebwerks bzw. des Lagers (7) änderbar ist.7. Lubrication system according to one of claims 1 to 6,
characterized in that the cycle of the metering device (5) can be changed by a control device (1), preferably as a function of several operating parameters of the gas turbine engine or of the bearing (7). 8. Schmiersystem nach einem der Ansprüche 1 bis 7,
dadurch gekennzeichnet, daß der Schmierstoff in Fluß­richtung zur Dosiereinrichtung (5) eine Heizeinrichtung (4) durchströmt.8. Lubrication system according to one of claims 1 to 7,
characterized in that the lubricant flows through a heating device (4) in the direction of flow to the metering device (5). 9. Schmiersystem nach einem der Ansprüche 1 bis 8,
dadurch gekennzeichnet, daß der Abfluß (24) in einen Schmierstoffabscheider (15) mündet und die austretende Druckluft in den Abgasschacht der Gasturbine abgeleitet ist.9. Lubrication system according to one of claims 1 to 8,
characterized in that the drain (24) opens into a lubricant separator (15) and the escaping compressed air is discharged into the exhaust gas shaft of the gas turbine. 10. Schmiersystem nach einem der Ansprüche 1 bis 9. dadurch gekennzeichnet, daß das Schmiermittel durch den Lagerinnenring der Lagerstelle (7) zugeführt ist.10. Lubrication system according to one of claims 1 to 9, characterized in that the lubricant is supplied through the bearing inner ring of the bearing point (7).
EP87116288A 1986-11-06 1987-11-05 Lubrication system for a gas turbine engine Expired - Lifetime EP0266765B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3637776 1986-11-06
DE19863637776 DE3637776A1 (en) 1986-11-06 1986-11-06 LUBRICATION SYSTEM FOR A GAS TURBINE ENGINE

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EP0266765A2 true EP0266765A2 (en) 1988-05-11
EP0266765A3 EP0266765A3 (en) 1989-03-22
EP0266765B1 EP0266765B1 (en) 1991-05-02

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DE (2) DE3637776A1 (en)

Cited By (4)

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US5268449A (en) * 1992-11-16 1993-12-07 Phillips Petroleum Company Random copolymers of poly(arylene sulfide)s and process therefor
WO2010136579A1 (en) * 2009-05-28 2010-12-02 Gea Westfalia Separator Gmbh Centrifuge having a lubricant system
CN103433867A (en) * 2013-08-20 2013-12-11 江苏经纬轨道交通设备有限公司 Lubricating grease injection tool for bearing
EP3418505A1 (en) * 2017-06-23 2018-12-26 HS Marston Aerospace Limited Heated lubrication circuit

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DE19852768A1 (en) * 1998-11-16 2000-05-18 Bmw Rolls Royce Gmbh Small gas turbine with a radial or Slinger combustion chamber
CN103032666A (en) * 2012-12-28 2013-04-10 南车株洲电机有限公司 Bearing lubricating grease filling device and filling method
DE102015218813A1 (en) 2015-09-29 2017-03-30 Bielomatik Leuze Gmbh + Co. Kg Lubrication device and method for lubricating machine parts

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US5268449A (en) * 1992-11-16 1993-12-07 Phillips Petroleum Company Random copolymers of poly(arylene sulfide)s and process therefor
WO2010136579A1 (en) * 2009-05-28 2010-12-02 Gea Westfalia Separator Gmbh Centrifuge having a lubricant system
US9186686B2 (en) 2009-05-28 2015-11-17 GEA Mechanical Equiptment GmbH Centrifuge having a lubricant system that delivers lubricant in temporally discrete pulses
CN103433867A (en) * 2013-08-20 2013-12-11 江苏经纬轨道交通设备有限公司 Lubricating grease injection tool for bearing
EP3418505A1 (en) * 2017-06-23 2018-12-26 HS Marston Aerospace Limited Heated lubrication circuit
US11136908B2 (en) 2017-06-23 2021-10-05 Hs Marston Aerospace Limited Heated lubrication circuit

Also Published As

Publication number Publication date
DE3637776A1 (en) 1988-05-11
DE3769754D1 (en) 1991-06-06
EP0266765A3 (en) 1989-03-22
EP0266765B1 (en) 1991-05-02

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